Due to physical/power/financial constraints of CubeSats, classical improvements of reliability in area of satellite avionics and data-handling (i.e. redundant subsystems, cross-strapping) are not usually possible. On top of that, CubeSat development rarely follows technical standards, and is usually based on COTS solutions additionally questioning reliability figures.This article proposes the use of concepts implemented usually on "bigger" satellites migrated into the world of CubeSat applications. Those concepts are described in SAVOIR working group, which standardises certain data-handling functionalities expected to be present in "mature" satellite. By applying specific engineering solutions and guidelines, most of the SAVOIR functions can be implemented in CubeSat, therefore increasing the reliability.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Standardization concepts for CubeSat applications


    Beteiligte:


    Erscheinungsdatum :

    02.10.2023


    Format / Umfang :

    3724641 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    CUBESAT ELECTRICAL INTERFACE STANDARDIZATION TO ACHIEVE FASTER DELIVERY AND MISSION SUCCESS

    Cho, Mengu / Yamauch, Takashi / Sejera, Marloun et al. | TIBKAT | 2021


    6U CubeSat commercial applications

    Tsitas, S R | Online Contents | 2012


    CUBESAT INTERFACE STANDARDIZATION TO ACHIEVE FASTER DELIVERY, MISSION SUCCESS AND MASS PRODUCTION

    Cho, Mengu / Takashi, Yamauchi / Sejera, Marloun et al. | TIBKAT | 2022


    Concepts for an Enhanced CubeSat GEO Space Situational Awareness Architecture

    Morris, Keith | British Library Conference Proceedings | 2014


    Terminology of fundamental standardization concepts

    Gutmann, I. | Engineering Index Backfile | 1933